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Rectangular Tank Calculation
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Rectangular Tank Calculation Sheet
TANK CALCULATION SHEET
I. DESIGN PARAMETERS:
- Code Design : API 650 & Roark's Formulas
- Design pressure Pd : Full water + 5 kPag
= 22.27 kPa
- Design temperature : 60oC / AMB
- Operating pressure : ATM
- Operating temperature : 27oC
- Corrosion Allowance C.A : 0 mm
- Liquid Specific Gravity : 1.00
- Joint Efficiency : 0.85 (For Shell)
: 1.00 (For Roof & Bottom)
- Elastic Modulus E : 2.9*E+7 psi
= 199947962 kPa
retangular
MATERIAL SPECIFICATION: :
- Shell, Roof & Bottom : SS 316L
- Allowable Stress Sa : 16700 psi
= 115142 kPa
- Nozzle Neck : A 182 F 316L
- Flange : A 182 F 316L
- Pipe Fittings : A 312 TP 316L
- Bolts & Nuts : A 193 Gr B8M / A 194 Gr 8M
- Stiffeners : SS 316L
TANK GEOMETRY:
- Height H : 1760 mm
- Length L : 1219 mm
- Width W : 1066 mm
II. DESIGN
Width (W)
Hei
ght
(H)
Page 1 of 28
Rectangular Tank Calculation Sheet
II.1 Side Wall Plate Calculation (Height x Length)
II.1.1 Wall Thickness Calculation
(As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
Vertical length without reinforced a : 587 mm
Horizontal length without reinforced b : 406 mm
Ratio, a/b : 1.44
α = 0.0797
β = 0.4658
Required thickness
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 3.86 mm
Adopted thickness ta : 6.00 mm
Maximum deflection
Ymax = α*Pd*b4/(E*ta
3) = 1.12 mm
Ymax < 1/2 ta
1.12mm < 3mm
Therefore, adopted thickness is satisfactory
II.1.2 Top Edge Stiffener
R1 = 0.03*Pd*a = 0.39 kN/m
R2 = 0.32*Pd*a = 4.18 kN/m
Moment inertia required:
Jmin = R1*b4/(192*E*ta) = 46.38 mm
4
= 0.0046 cm4
Moment inertia of used stiffener (Flat bar 65x6):
Jx = Jy = 13.7 cm4
Therefore, Top edge stiffener is satisfactory
II.1.3 Horizontal Stiffener
Moment inertia required:
Jmin = R2*b4/(192*E*ta) = 494.69 mm
4
= 0.0495 cm4
Moment inertia of used stiffener (Flat bar 65x6):
Jx = Jy = 13.7 cm4
Therefore, Horizontal stiffener is satisfactory
II.1.4 Vertical Stiffener
Hei
ght
(H)
a
b
Length (L)
a
b
Stiffeners
a
b
a
b
Page 2 of 28
Rectangular Tank Calculation Sheet
Maximum bending moment at Hy = 0.5773*amax = 338.68 mm
Maximum bending moment:
Mmax = 0.0641*Pd*b*Hy2
= 0.07 kNm
Required section modulus:
Zr = Mmax/Sa = 5.78E-07 mm3
= 0.58 cm3
Section modulus of used stiffener (Flat bar 65x6):
Z = 4.2 cm3
Therefore, Vertical stiffener is satisfactory
II.2 Side Wall Plate Calculation (Height x Width)
II.2.1 Wall Thickness Calculation
(As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
Vertical length without reinforced a : 587 mm
Horizontal length without reinforced b : 355 mm
Ratio, a/b : 1.65
α = 0.0934
β = 0.5301
Required thickness
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 3.60 mm
Adopted thickness ta : 6.00 mm
Maximum deflection
Ymax = α*Pd*b4/(E*ta
3) = 0.77 mm
Ymax < 1/2 ta
0.77mm < 3mm
Therefore, adopted thickness is satisfactory
II.2.2 Top Edge Stiffener
R1 = 0.03*Pd*a = 0.39 kN/m
R2 = 0.32*Pd*a = 4.18 kN/m
Moment inertia required:
Jmin = R1*b4/(192*E*ta) = 27.12 mm
4
= 0.0027 cm4
Moment inertia of used stiffener (Flat bar 65x6):
Jx = Jy = 13.7 cm4
Therefore, Top edge stiffener is satisfactory
II.2.3 Horizontal Stiffener
Hei
ght
(H
)
a
b
a
b
Stiffeners
a
b
a
b
Width (W)
Page 3 of 28
Rectangular Tank Calculation Sheet
Moment inertia required:
Jmin = R2*b4/(192*E*ta) = 289.30 mm
4
= 0.0289 cm4
Moment inertia of used stiffener (Flat bar 65x6):
Jx = Jy = 13.7 cm4
Therefore, Horizontal stiffener is satisfactory
II.2.4 Vertical Stiffener
Maximum bending moment at Hy = 0.5773*amax = 338.68 mm
Maximum bending moment:
Mmax = 0.0641*Pd*b*Hy2
= 0.06 kNm
Required section modulus:
Zr = Mmax/Sa = 5.05E-07 mm3
= 0.51 cm3
Section modulus of used stiffener (Flat bar 65x6):
Z = 4.2 cm3
Therefore, Vertical stiffener is satisfactory
II.3 Roof Plate Calculation
Loads on roof plate:
- Roof area: = 1.299454 m2
- Live load: = 1.5 kPa
- Roof weight: = 111 kg
- Roof structure weight: = 116 kg
- Roof Equipment weight: = 120 kg
- Dead load: = 2.6 kPa
Total load on roof plate: = 4.1 kPa
Distance without reinforced in width a : 533 mm
Distance without reinforced in length b : 609.5 mm
Ratio, a/b : 0.87
α = 0.0332
β = 0.2297
Required thickness:
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 1.75 mm
Adopted thickness ta : 6.00 mm
Maximum deflection:
Ymax = α*Pd*b4/(E*ta
3) = 0.44 mm
Ymax < 1/2 ta
0.44mm < 3mm
Therefore, adopted thickness is satisfactory
II.4 Bottom Plate Calculation
Stiffeners
Wid
th (
W)
Length (L)
aa
bb
a
b
a
b
Stiffeners
a
b
a
b
Wid
th (
W)
Length (L)
Page 4 of 28
Rectangular Tank Calculation Sheet
Distance without reinforced in width a : 533 mm
Distance without reinforced in length b : 609.5 mm
Ratio, a/b : 0.87
α = 0.0332
β = 0.2297
Required thickness:
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 4.06 mm
Adopted thickness ta : 8.00 mm
Maximum deflection:
Ymax = α*Pd*b4/(E*ta
3) = 1.00 mm
Ymax < 1/2 ta
1mm < 4mm
Therefore, adopted thickness is satisfactory
a
b
a
b
Stiffeners
a
b
a
b
Wid
th (
W)
Length (L)
Page 5 of 28
Rectangular Tank Calculation Sheet
TANK CALCULATION SHEET
I. DESIGN PARAMETERS:
- Code Design : API 650 & Roark's Formulas
- Design pressure Pd : Full water + 5 kPag
= 24.62 kPa
- Design temperature : 60oC / AMB
- Operating pressure : ATM
- Operating temperature : 27oC
- Corrosion Allowance C.A : 0 mm
- Liquid Specific Gravity : 1.00
- Joint Efficiency : 0.85 (For Shell)
: 1.00 (For Roof & Bottom)
- Elastic Modulus E : 2.9*E+7 psi
= 199947962 kPa
retangular
MATERIAL SPECIFICATION: :
- Shell, Roof & Bottom : SS 316L
- Allowable Stress Sa : 16700 psi
= 115142 kPa
- Nozzle Neck : A 182 F 316L
- Flange : A 182 F 316L
- Pipe Fittings : A 312 TP 316L
- Bolts & Nuts : A 193 Gr B8M / A 194 Gr 8M
- Stiffeners : SS 316L
TANK GEOMETRY:
- Height H : 2000 mm
- Length L : 5600 mm
- Width W : 1100 mm
Width (W)
Hei
ght
(H)
Page 6 of 28
Rectangular Tank Calculation Sheet
II. DESIGN
II.1 Side Wall Plate Calculation (Height x Length)
II.1.1 Wall Thickness Calculation
(As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
Vertical length without reinforced a : 667 mm
Horizontal length without reinforced b : 622 mm
Ratio, a/b : 1.07
α = 0.0504
β = 0.3185
Required thickness
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 5.13 mm
Adopted thickness ta : 8.00 mm
Maximum deflection
Ymax = α*Pd*b4/(E*ta
3) = 1.82 mm
Ymax < 1/2 ta
1.82mm < 4mm
Therefore, adopted thickness is satisfactory
II.1.2 Top Edge Stiffener
R1 = 0.03*Pd*a = 0.49 kN/m
R2 = 0.32*Pd*a = 5.25 kN/m
Moment inertia required:
Jmin = R1*b4/(192*E*ta) = 240.32 mm
4
= 0.0240 cm4
Moment inertia of used stiffener (angle 65x65x6):
Jx = Jy = 29.4 cm4
Therefore, Top edge stiffener is satisfactory
II.1.3 Horizontal Stiffener
Moment inertia required:
Jmin = R2*b4/(192*E*ta) = 2563.43 mm
4
= 0.2563 cm4
Moment inertia of used stiffener (angle 65x65x6):
Jx = Jy = 29.4 cm4
Therefore, Horizontal stiffener is satisfactory
Hei
ght
(H)
a
b
Length (L)
a
b
Stiffeners
a
b
a
b
Page 7 of 28
Rectangular Tank Calculation Sheet
II.1.4 Vertical Stiffener
Maximum bending moment at Hy = 0.5773*amax = 384.87 mm
Maximum bending moment:
Mmax = 0.0641*Pd*b*Hy2
= 0.15 kNm
Required section modulus:
Zr = Mmax/Sa = 1.26E-06 mm3
= 1.26 cm3
Section modulus of used stiffener (angle 65x65x6):
Z = 6.26 cm3
Therefore, Vertical stiffener is satisfactory
II.2 Side Wall Plate Calculation (Height x Width)
II.2.1 Wall Thickness Calculation
(As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
Vertical length without reinforced a : 667 mm
Horizontal length without reinforced b : 550 mm
Ratio, a/b : 1.21
α = 0.0624
β = 0.38
Required thickness
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 4.96 mm
Adopted thickness ta : 8.00 mm
Maximum deflection
Ymax = α*Pd*b4/(E*ta
3) = 1.37 mm
Ymax < 1/2 ta
1.37mm < 4mm
Therefore, adopted thickness is satisfactory
II.2.2 Top Edge Stiffener
R1 = 0.03*Pd*a = 0.49 kN/m
R2 = 0.32*Pd*a = 5.25 kN/m
Moment inertia required:
Jmin = R1*b4/(192*E*ta) = 146.71 mm
4
= 0.0147 cm4
Moment inertia of used stiffener (angle 65x65x6):
Jx = Jy = 29.4 cm4
Therefore, Top edge stiffener is satisfactory
Hei
ght
(H
)
a
b
a
b
Stiffeners
a
b
a
b
Width (W)
Page 8 of 28
Rectangular Tank Calculation Sheet
II.2.3 Horizontal Stiffener
Moment inertia required:
Jmin = R2*b4/(192*E*ta) = 1564.91 mm
4
= 0.1565 cm4
Moment inertia of used stiffener (angle 65x65x6):
Jx = Jy = 29.4 cm4
Therefore, Horizontal stiffener is satisfactory
II.2.4 Vertical Stiffener
Maximum bending moment at Hy = 0.5773*amax = 384.87 mm
Maximum bending moment:
Mmax = 0.0641*Pd*b*Hy2
= 0.13 kNm
Required section modulus:
Zr = Mmax/Sa = 1.12E-06 mm3
= 1.12 cm3
Section modulus of used stiffener (angle 65x65x6):
Z = 6.26 cm3
Therefore, Vertical stiffener is satisfactory
II.3 Roof Plate Calculation
Loads on roof plate:
- Roof area: = 6.16 m2
- Live load: = 1.5 kPa
- Roof weight: = 340 kg
- Roof structure weight: = 116 kg
- Roof Equipment weight: = 120 kg
- Dead load: = 0.9 kPa
Total load on roof plate: = 2.4 kPa
Distance without reinforced in width a : 1100 mm
Distance without reinforced in length b : 700 mm
Ratio, a/b : 1.57
α = 0.0886
β = 0.5076
Required thickness:
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 2.29 mm
Adopted thickness ta : 6.00 mm
Maximum deflection:
Ymax = α*Pd*b4/(E*ta
3) = 1.19 mm
Ymax < 1/2 ta
1.19mm < 3mm
Therefore, adopted thickness is satisfactory
Stiffeners
Wid
th (
W)
Length (L)
aa
bb
Page 9 of 28
Rectangular Tank Calculation Sheet
II.4 Bottom Plate Calculation
Distance without reinforced in width a : 550 mm
Distance without reinforced in length b : 622 mm
Ratio, a/b : 0.88
α = 0.0341
β = 0.2341
Required thickness:
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 4.40 mm
Adopted thickness ta : 8.00 mm
Maximum deflection:
Ymax = α*Pd*b4/(E*ta
3) = 1.23 mm
Ymax < 1/2 ta
1.23mm < 4mm
Therefore, adopted thickness is satisfactory
a
b
a
b
Stiffeners
a
b
a
b
Wid
th (
W)
Length (L)
Page 10 of 28
Rectangular Tank Calculation Sheet
TANK CALCULATION SHEET
I. DESIGN PARAMETERS:
- Code Design : API 650 & Roark's Formulas
- Design pressure Pd : Full water + 5 kPag
= 24.62 kPa
- Design temperature : 60oC / AMB
- Operating pressure : ATM
- Operating temperature : 27oC
- Corrosion Allowance C.A : 0 mm
- Liquid Specific Gravity : 1.00
- Joint Efficiency : 0.85 (For Shell)
: 1.00 (For Roof & Bottom)
- Elastic Modulus E : 2.9*E+7 psi
= 199947962 kPa
retangular
MATERIAL SPECIFICATION: :
- Shell, Roof & Bottom : SS 316L
- Allowable Stress Sa : 16700 psi
= 115142 kPa
- Nozzle Neck : A 182 F 316L
- Flange : A 182 F 316L
- Pipe Fittings : A 312 TP 316L
- Bolts & Nuts : A 193 Gr B8M / A 194 Gr 8M
- Stiffeners : SS 316L
TANK GEOMETRY:
- Height H : 2000 mm
- Length L : 5700 mm
- Width W : 1250 mm
Width (W)
Hei
ght
(H)
Page 11 of 28
Rectangular Tank Calculation Sheet
II. DESIGN
II.1 Side Wall Plate Calculation (Height x Length)
II.1.1 Wall Thickness Calculation
(As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
Vertical length without reinforced a : 667 mm
Horizontal length without reinforced b : 633 mm
Ratio, a/b : 1.05
α = 0.0487
β = 0.3096
Required thickness
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 5.15 mm
Adopted thickness ta : 8.00 mm
Maximum deflection
Ymax = α*Pd*b4/(E*ta
3) = 1.88 mm
Ymax < 1/2 ta
1.88mm < 4mm
Therefore, adopted thickness is satisfactory
II.1.2 Top Edge Stiffener
R1 = 0.03*Pd*a = 0.49 kN/m
R2 = 0.32*Pd*a = 5.25 kN/m
Moment inertia required:
Jmin = R1*b4/(192*E*ta) = 257.95 mm
4
= 0.0258 cm4
Moment inertia of used stiffener (angle 65x65x6):
Jx = Jy = 29.4 cm4
Therefore, Top edge stiffener is satisfactory
II.1.3 Horizontal Stiffener
Moment inertia required:
Jmin = R2*b4/(192*E*ta) = 2751.49 mm
4
= 0.2751 cm4
Moment inertia of used stiffener (angle 65x65x6):
Jx = Jy = 29.4 cm4
Therefore, Horizontal stiffener is satisfactory
Hei
ght
(H)
a
b
Length (L)
a
b
Stiffeners
a
b
a
b
Page 12 of 28
Rectangular Tank Calculation Sheet
II.1.4 Vertical Stiffener
Maximum bending moment at Hy = 0.5773*amax = 384.87 mm
Maximum bending moment:
Mmax = 0.0641*Pd*b*Hy2
= 0.15 kNm
Required section modulus:
Zr = Mmax/Sa = 1.29E-06 mm3
= 1.29 cm3
Section modulus of used stiffener (angle 65x65x6):
Z = 6.26 cm3
Therefore, Vertical stiffener is satisfactory
II.2 Side Wall Plate Calculation (Height x Width)
II.2.1 Wall Thickness Calculation
(As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
Vertical length without reinforced a : 667 mm
Horizontal length without reinforced b : 625 mm
Ratio, a/b : 1.07
α = 0.0504
β = 0.3185
Required thickness
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 5.16 mm
Adopted thickness ta : 8.00 mm
Maximum deflection
Ymax = α*Pd*b4/(E*ta
3) = 1.85 mm
Ymax < 1/2 ta
1.85mm < 4mm
Therefore, adopted thickness is satisfactory
II.2.2 Top Edge Stiffener
R1 = 0.03*Pd*a = 0.49 kN/m
R2 = 0.32*Pd*a = 5.25 kN/m
Moment inertia required:
Jmin = R1*b4/(192*E*ta) = 244.64 mm
4
= 0.0245 cm4
Moment inertia of used stiffener (angle 65x65x6):
Jx = Jy = 29.4 cm4
Therefore, Top edge stiffener is satisfactory
Hei
ght
(H
)
a
b
a
b
Stiffeners
a
b
a
b
Width (W)
Page 13 of 28
Rectangular Tank Calculation Sheet
II.2.3 Horizontal Stiffener
Moment inertia required:
Jmin = R2*b4/(192*E*ta) = 2609.51 mm
4
= 0.2610 cm4
Moment inertia of used stiffener (angle 65x65x6):
Jx = Jy = 29.4 cm4
Therefore, Horizontal stiffener is satisfactory
II.2.4 Vertical Stiffener
Maximum bending moment at Hy = 0.5773*amax = 384.87 mm
Maximum bending moment:
Mmax = 0.0641*Pd*b*Hy2
= 0.15 kNm
Required section modulus:
Zr = Mmax/Sa = 1.27E-06 mm3
= 1.27 cm3
Section modulus of used stiffener (angle 65x65x6):
Z = 6.26 cm3
Therefore, Vertical stiffener is satisfactory
II.3 Roof Plate Calculation
Loads on roof plate:
- Roof area: = 7.125 m2
- Live load: = 1.5 kPa
- Roof weight: = 386 kg
- Roof structure weight: = 116 kg
- Roof Equipment weight: = 120 kg
- Dead load: = 0.9 kPa
Total load on roof plate: = 2.4 kPa
Distance without reinforced in width a : 1250 mm
Distance without reinforced in length b : 712.5 mm
Ratio, a/b : 1.75
α = 0.0989
β = 0.5559
Required thickness:
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 2.40 mm
Adopted thickness ta : 6.00 mm
Maximum deflection:
Ymax = α*Pd*b4/(E*ta
3) = 1.39 mm
Ymax < 1/2 ta
1.39mm < 3mm
Therefore, adopted thickness is satisfactory
Stiffeners
Wid
th (
W)
Length (L)
aa
bb
Page 14 of 28
Rectangular Tank Calculation Sheet
II.4 Bottom Plate Calculation
Distance without reinforced in width a : 625 mm
Distance without reinforced in length b : 633 mm
Ratio, a/b : 0.99
α = 0.0435
β = 0.283
Required thickness:
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 4.93 mm
Adopted thickness ta : 8.00 mm
Maximum deflection:
Ymax = α*Pd*b4/(E*ta
3) = 1.68 mm
Ymax < 1/2 ta
1.68mm < 4mm
Therefore, adopted thickness is satisfactory
a
b
a
b
Stiffeners
a
b
a
b
Wid
th (
W)
Length (L)
Page 15 of 28
Rectangular Tank Calculation Sheet
TANK CALCULATION SHEET
I. DESIGN PARAMETERS:
- Code Design : API 650 & Roark's Formulas
- Design pressure Pd : Full water + 5 kPag
= 24.62 kPa
- Design temperature : 60oC / AMB
- Operating pressure : ATM
- Operating temperature : 27oC
- Corrosion Allowance C.A : 0 mm
- Liquid Specific Gravity : 1.00
- Joint Efficiency : 0.85 (For Shell)
: 1.00 (For Roof & Bottom)
- Elastic Modulus E : 2.9*E+7 psi
= 199947962 kPa
retangular
MATERIAL SPECIFICATION: :
- Shell, Roof & Bottom : SS 316L
- Allowable Stress Sa : 16700 psi
= 115142 kPa
- Nozzle Neck : A 182 F 316L
- Flange : A 182 F 316L
- Pipe Fittings : A 312 TP 316L
- Bolts & Nuts : A 193 Gr B8M / A 194 Gr 8M
- Stiffeners : SS 316L
TANK GEOMETRY:
- Height H : 2000 mm
- Length L : 2100 mm
- Width W : 1250 mm
II. DESIGN
Width (W)
Hei
ght
(H)
Page 16 of 28
Rectangular Tank Calculation Sheet
II.1 Side Wall Plate Calculation (Height x Length)
II.1.1 Wall Thickness Calculation
(As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
Vertical length without reinforced a : 500.0 mm
Horizontal length without reinforced b : 525 mm
Ratio, a/b : 0.95
α = 0.0401
β = 0.2652
Required thickness
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 3.95 mm
Adopted thickness ta : 6.00 mm
Maximum deflection
Ymax = α*Pd*b4/(E*ta
3) = 1.74 mm
Ymax < 1/2 ta
1.74mm < 3mm
Therefore, adopted thickness is satisfactory
II.1.2 Top Edge Stiffener
R1 = 0.03*Pd*a = 0.37 kN/m
R2 = 0.32*Pd*a = 3.94 kN/m
Moment inertia required:
Jmin = R1*b4/(192*E*ta) = 121.80 mm
4
= 0.0122 cm4
Moment inertia of used stiffener (Flat bar 65x6):
Jx = Jy = 13.7 cm4
Therefore, Top edge stiffener is satisfactory
II.1.3 Horizontal Stiffener
Moment inertia required:
Jmin = R2*b4/(192*E*ta) = 1299.20 mm
4
= 0.1299 cm4
Moment inertia of used stiffener (Flat bar 65x6):
Jx = Jy = 13.7 cm4
Therefore, Horizontal stiffener is satisfactory
II.1.4 Vertical Stiffener
Hei
ght
(H)
a
b
Length (L)
a
b
Stiffeners
a
b
a
b
Page 17 of 28
Rectangular Tank Calculation Sheet
Maximum bending moment at Hy = 0.5773*amax = 288.65 mm
Maximum bending moment:
Mmax = 0.0641*Pd*b*Hy2
= 0.07 kNm
Required section modulus:
Zr = Mmax/Sa = 6.00E-07 mm3
= 0.60 cm3
Section modulus of used stiffener (Flat bar 65x6):
Z = 4.2 cm3
Therefore, Vertical stiffener is satisfactory
II.2 Side Wall Plate Calculation (Height x Width)
II.2.1 Wall Thickness Calculation
(As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
Vertical length without reinforced a : 500 mm
Horizontal length without reinforced b : 417 mm
Ratio, a/b : 1.20
α = 0.0616
β = 0.3762
Required thickness
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 3.74 mm
Adopted thickness ta : 6.00 mm
Maximum deflection
Ymax = α*Pd*b4/(E*ta
3) = 1.06 mm
Ymax < 1/2 ta
1.06mm < 3mm
Therefore, adopted thickness is satisfactory
II.2.2 Top Edge Stiffener
R1 = 0.03*Pd*a = 0.37 kN/m
R2 = 0.32*Pd*a = 3.94 kN/m
Moment inertia required:
Jmin = R1*b4/(192*E*ta) = 48.32 mm
4
= 0.0048 cm4
Moment inertia of used stiffener (Flat bar 65x6):
Jx = Jy = 13.7 cm4
Therefore, Top edge stiffener is satisfactory
II.2.3 Horizontal Stiffener
Hei
ght
(H
)
a
b
a
b
Stiffeners
a
b
a
b
Width (W)
Page 18 of 28
Rectangular Tank Calculation Sheet
Moment inertia required:
Jmin = R2*b4/(192*E*ta) = 515.46 mm
4
= 0.0515 cm4
Moment inertia of used stiffener (Flat bar 65x6):
Jx = Jy = 13.7 cm4
Therefore, Horizontal stiffener is satisfactory
II.2.4 Vertical Stiffener
Maximum bending moment at Hy = 0.5773*amax = 288.65 mm
Maximum bending moment:
Mmax = 0.0641*Pd*b*Hy2
= 0.05 kNm
Required section modulus:
Zr = Mmax/Sa = 4.76E-07 mm3
= 0.48 cm3
Section modulus of used stiffener (Flat bar 65x6):
Z = 4.2 cm3
Therefore, Vertical stiffener is satisfactory
II.3 Roof Plate Calculation
Loads on roof plate:
- Roof area: = 2.625 m2
- Live load: = 1.5 kPa
- Roof weight: = 174 kg
- Roof structure weight: = 116 kg
- Roof Equipment weight: = 120 kg
- Dead load: = 1.5 kPa
Total load on roof plate: = 3.0 kPa
Distance without reinforced in width a : 1250 mm
Distance without reinforced in length b : 700 mm
Ratio, a/b : 1.79
α = 0.1011
β = 0.5662
Required thickness:
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 2.70 mm
Adopted thickness ta : 6.00 mm
Maximum deflection:
Ymax = α*Pd*b4/(E*ta
3) = 1.70 mm
Ymax < 1/2 ta
1.7mm < 3mm
Therefore, adopted thickness is satisfactory
II.4 Bottom Plate Calculation
Stiffeners
Wid
th (
W)
Length (L)
aa
bb
a
b
a
b
Stiffeners
a
b
a
b
Wid
th (
W)
Length (L)
Page 19 of 28
Rectangular Tank Calculation Sheet
Distance without reinforced in width a : 625 mm
Distance without reinforced in length b : 525 mm
Ratio, a/b : 1.19
α = 0.0607
β = 0.3718
Required thickness:
tr = Sqrt(β*Pd*b2)/Sa) + C.A = 4.68 mm
Adopted thickness ta : 8.00 mm
Maximum deflection:
Ymax = α*Pd*b4/(E*ta
3) = 1.11 mm
Ymax < 1/2 ta
1.11mm < 4mm
Therefore, adopted thickness is satisfactory
a
b
a
b
Stiffeners
a
b
a
b
Wid
th (
W)
Length (L)
Page 20 of 28
THANG LONG
ITEM NO. NAME
DESIGN CAPACITY
(m3)
LENGTH
(mm)
WIDTH
(mm)
HEIGHT
(mm)
T-6601 CORROSION INHIBITOR TANK 2.22 1219 1066 1760
T-6603 POUR POINT DEPRESSANT TANK 12.02 5600 1100 2000
T-6605 BACK UP CHEMICAL TANK 2.22 1219 1066 1760
T-6607 DEMULSIFIER TANK 2.22 1219 1066 1760
T-6621 CORROSION INHIBITOR TANK 2.22 1219 1066 1760
T-6622 POUR POINT DEPRESSANT TANK 13.93 5700 1250 2000
T-6623 DEMULSIFIER TANK 2.22 1219 1066 1760
T-6624 H2S SCAVENGER TANK 5.13 2100 1250 2000
T-6629 BACK UP CHEMICAL TANK 2.22 1219 1066 1760
T-6636 SCALE INHIBITOR TANK 2.22 1219 1066 1760
DONG DO
HEIGHT X LENGTH HEIGHT X WIDTH ROOF PLATE BOTTOM PLATE
t
(mm)
a
(mm)
b
(mm)
t
(mm)
a
(mm)
b
(mm)
t
(mm)
a
(mm)
b
(mm)
t
(mm)
a
(mm)
b
(mm)
6 587 406 6 587 355 6 533 609.5 8 533 609.5
8 667 700 8 667 550 6 1100 700 8 550 700
6 587 406 6 587 355 6 533 609.5 8 533 609.5
6 587 406 6 587 355 6 533 609.5 8 533 609.5
6 587 406 6 587 355 6 533 609.5 8 533 609.5
8 667 712.5 8 667 625 6 1250 712.5 8 625 712.5
6 587 406 6 587 355 6 533 609.5 8 533 609.5
6 500 525 6 500 417 6 1250 700 8 625 700
6 587 406 6 587 355 6 533 609.5 8 533 609.5
6 587 406 6 587 355 6 533 609.5 8 533 609.5
A(L)
(mm2)
A(U)
(mm2)
binh
(kg)
tang cung
(kg)mw nozz accessary
Base
framedry
specific
gravity
4 4 4 4 3 3 3 3 390 1160 517 119 63 20 20 53 792 0.99
4 10 4 3 2 9 3 10 753 1160 2344 766 63 20 20 144 3357 0.91
4 4 4 4 3 3 3 3 390 1160 517 119 63 20 20 53 792 0.781
4 4 4 4 3 3 3 3 390 1160 517 119 63 20 20 53 792 1.02
4 4 4 4 3 3 3 3 390 1160 517 119 63 20 20 53 792 0.99
4 10 4 3 2 9 3 10 753 1160 2513 776 63 20 20 148 3541 0.91
4 4 4 4 3 3 3 3 390 1160 517 119 63 20 20 53 792 1.02
5 5 5 4 2 4 3 5 390 1160 913 195 63 20 20 77 1289 0.998
4 4 4 4 3 3 3 3 390 1160 517 119 63 20 20 53 792 0.78
4 4 4 4 3 3 3 3 390 1160 517 119 63 20 20 53 792 1.3
capacity
working
luu chat
(kg)operating
hydro
test
2 1980 2772 3013
10.85 9873.5 13231 15379
2 1562 2354 3013
2 2040 2832 3013
2 1980 2772 3013
12.63 11493.3 15034 17471
2 2040 2832 3013
4.6 4590.8 5879 6422
2 1560 2352 3013
2 2600 3392 3013